CN211639611U - Supporting device for airplane part machining - Google Patents
Supporting device for airplane part machining Download PDFInfo
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- CN211639611U CN211639611U CN201922442834.9U CN201922442834U CN211639611U CN 211639611 U CN211639611 U CN 211639611U CN 201922442834 U CN201922442834 U CN 201922442834U CN 211639611 U CN211639611 U CN 211639611U
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Abstract
The utility model provides an aircraft strutting arrangement for parts machining, belongs to the fixed technical field of aircraft special type part, including unable adjustment base, activity carousel, fixed extension board, locking jackscrew, activity commentaries on classics piece, adjusting device, fixing device, its characterized in that: the adjustable rotary table is characterized in that a movable rotary table is inserted in the center of the circle of the top end surface of the fixed base, a fixed support plate is fixedly connected to the left edge of the top end surface of the movable rotary table, a locking jackscrew is inserted in the middle of the upper portion of the left top end surface of the fixed support plate, a movable rotary block is connected to the middle of the upper portion of the top end surface of the right side of the fixed support plate, an adjusting device is fixedly connected to the middle of the upper edge of the front top end surface of the movable rotary block, a fixing device is fixedly connected to the middle of the rear edge of the top end surface of the movable rotary block, a worker can quickly adjust the angle of the fixator at any.
Description
The technical field is as follows:
the utility model belongs to the technical field of the fixed apparatus of aircraft part, concretely relates to strutting arrangement is used in aircraft parts machining.
Background art:
in long-term work practice, during the staff will irregular aircraft part fixing process, current fixer needs the staff to prepare every try on of the fixer of a plurality of different angles to current fixer is unsettled form and is out of shape very easily behind the fixed part circular arc department, and inconvenient staff operates and uses and reduces work efficiency.
The utility model has the following contents:
the utility model aims at: in order to solve the staff with the fixed in-process of irregular aircraft part, the staff is quick at any time adjusts the fixer angle to the staff can support the cambered surface below with unsettled man-hour and prevent to warp, makes things convenient for the staff to operate and use and improves work efficiency, and its technical scheme is as follows:
the utility model provides an aircraft strutting arrangement for parts machining, it includes unable adjustment base 1, activity carousel 2, fixed extension board 3, locking jackscrew 4, activity commentaries on classics piece 5, adjusting device 6, fixing device 7, its characterized in that: a movable turntable 2 is inserted in the center of the circle on the top surface of the fixed base 1, a fixed support plate 3 is fixedly connected to the left edge of the top surface of the movable turntable 2, a locking jackscrew 4 is inserted in the middle of the top surface of the left end of the fixed support plate 3, a movable rotating block 5 is connected to the middle of the top surface of the right side of the fixed support plate 3, an adjusting device 6 is fixedly connected to the middle of the upper edge of the front top surface of the movable rotating block 5, a fixing device 7 is fixedly connected to the middle of the rear edge of the top surface of the movable rotating block 5, the fixed base 1 comprises a chassis 1-1, an insert ring 1-2 and a bearing 1-3, an insert ring 1-2 is fixedly connected to the center of the top surface of the chassis 1-1, a bearing 1-3 is fixedly inserted in the center of the circle in the insert ring 1-2, and the movable turntable 2 is inserted in the, the adjusting device 6 comprises a support block 6-1, a threaded column 6-2, a top column 6-3 and an adjusting disc 6-4, the threaded column 6-2 is inserted in the middle of the upper top end surface of the support block 6-1, the top column 6-3 is fixedly connected with the circle center of the upper top end surface of the threaded column 6-2, the adjusting disc 6-4 is fixedly connected with the circle center of the lower top end surface of the threaded column 6-2, the support block 6-1 is fixedly connected with the middle of the upper edge of the front top end surface of the movable rotating block 5, the fixing device 7 comprises a clamping block 7-1, a pressure plate 7-2 and a bolt 7-3, the clamping block 7-1 is in a concave shape, the pressure plate 7-2 is inserted above the inside of the clamping block 7-1, the bolt 7-3 is respectively inserted in the middle of the edge of the upper top end surface of the clamping block 7-1, the bolt 7-3 penetrates through the upper surface of the clamping block 7-1 and is inserted into the upper surface of the pressing plate 7-2.
The utility model has the advantages that: in order to solve the problem that an operator fixes irregular airplane parts, the angle of the fixing device can be quickly adjusted by the operator at any time, the operator can support the lower part of the suspended arc surface to prevent deformation during machining, and the fixing device is convenient for the operator to operate and use and improves the working efficiency.
Description of the drawings:
fig. 1 is a schematic view of the overall structure of the present invention;
fig. 2 is a schematic structural view of the fixing base 1 of the present invention;
fig. 3 is a schematic structural diagram of the adjusting device 6 of the present invention;
fig. 4 is a schematic structural diagram of the fixing device 7 of the present invention.
The specific implementation mode is as follows:
referring to fig. 1, fig. 2, fig. 3, fig. 4, the supporting device for aircraft part processing includes a fixed base 1, a movable turntable 2, a fixed support plate 3, a locking jackscrew 4, a movable rotating block 5, an adjusting device 6, and a fixing device 7, and is characterized in that: a movable turntable 2 is inserted in the center of the circle on the top surface of the fixed base 1, a fixed support plate 3 is fixedly connected to the left edge of the top surface of the movable turntable 2, a locking jackscrew 4 is inserted in the middle of the top surface of the left end of the fixed support plate 3, a movable rotating block 5 is connected to the middle of the top surface of the right side of the fixed support plate 3, an adjusting device 6 is fixedly connected to the middle of the upper edge of the front top surface of the movable rotating block 5, a fixing device 7 is fixedly connected to the middle of the rear edge of the top surface of the movable rotating block 5, the fixed base 1 comprises a chassis 1-1, an insert ring 1-2 and a bearing 1-3, an insert ring 1-2 is fixedly connected to the center of the top surface of the chassis 1-1, a bearing 1-3 is fixedly inserted in the center of the circle in the insert ring 1-2, and the movable turntable 2 is inserted in the, the adjusting device 6 comprises a support block 6-1, a threaded column 6-2, a top column 6-3 and an adjusting disc 6-4, the threaded column 6-2 is inserted in the middle of the upper top end surface of the support block 6-1, the top column 6-3 is fixedly connected with the circle center of the upper top end surface of the threaded column 6-2, the adjusting disc 6-4 is fixedly connected with the circle center of the lower top end surface of the threaded column 6-2, the support block 6-1 is fixedly connected with the middle of the upper edge of the front top end surface of the movable rotating block 5, the fixing device 7 comprises a clamping block 7-1, a pressure plate 7-2 and a bolt 7-3, the clamping block 7-1 is in a concave shape, the pressure plate 7-2 is inserted above the inside of the clamping block 7-1, the bolt 7-3 is respectively inserted in the middle of the edge of the upper top end surface of the clamping block 7-1, the bolt 7-3 penetrates through the upper surface of the clamping block 7-1 and is inserted into the upper surface of the pressing plate 7-2.
When in use, firstly, the chassis 1-1 on the auxiliary large team length 1 is placed on a processing table and fixed, then the edge of a workpiece is inserted into the clamping block 7-1 on the fixing device 7, simultaneously, the movable rotating disc 2 is rotated when the clamping block 7-1 is inserted into the edge of the workpiece, the movable rotating disc 2 is rotated in the bearing 1-3 in the insert ring 1-2 to adjust the left and right angles, the opening of the clamping block 7-1 is aligned with the edge of the workpiece to be conveniently inserted, simultaneously, the movable rotating block 5 is rotated on the side surface of the fixed support plate 3 by taking the locking jackscrew 4 as the circle center, the vertical angle of the clamping block 7-1 is adjusted, then, after the adjustment is finished, the locking jackscrew 4 is rotated to fix the movable rotating block 5 on the side surface of the fixed support plate 3, then the bolt 7-3 is rotated to move the bolt 7-3 downwards in the clamping block 7-1, then holding the adjusting disk 6-4 on the adjusting device 6 to move the threaded column 6-2 upwards on the support block 6-1, and finally contacting the top column 6-3 with the lower surface of the workpiece to support the workpiece to prevent deformation.
Of course, the above description is not intended to limit the present invention, and the present invention is not limited to the above examples, and the changes, modifications, additions or substitutions made by those skilled in the art within the scope of the present invention should also belong to the protection scope of the present invention.
Claims (4)
1. The utility model provides an aircraft strutting arrangement for parts machining, includes unable adjustment base (1), activity carousel (2), fixed extension board (3), locking jackscrew (4), activity commentaries on classics piece (5), adjusting device (6), fixing device (7), its characterized in that: the movable rotary table is characterized in that a movable rotary table (2) is inserted in the center of the circle of the top end surface of the fixed base (1), a fixed support plate (3) is fixedly connected to the left edge of the top end surface of the movable rotary table (2), a locking jackscrew (4) is inserted in the middle of the upper portion of the left top end surface of the fixed support plate (3), a movable rotary block (5) is connected to the middle of the upper portion of the right top end surface of the fixed support plate (3), an adjusting device (6) is fixedly connected to the middle of the upper edge of the front top end surface of the movable rotary block (5), and a fixing device (7) is fixedly connected to the middle of the rear edge of the.
2. The support device for aircraft parts machining according to claim 1, characterized in that: the fixed base (1) comprises a chassis (1-1), an inserting ring (1-2) and a bearing (1-3), wherein the inserting ring (1-2) is fixedly connected to the circle center of the surface of the top end of the chassis (1-1), the bearing (1-3) is fixedly inserted into the circle center of the inner portion of the inserting ring (1-2), and the movable rotary table (2) is inserted into the bearing (1-3).
3. The support device for aircraft parts machining according to claim 1, characterized in that: the adjusting device (6) comprises a support block (6-1), a threaded column (6-2), a top column (6-3) and an adjusting disc (6-4), the threaded column (6-2) is inserted in the middle of the upper top end surface of the support block (6-1), the top column (6-3) is fixedly connected to the circle center of the upper top end surface of the threaded column (6-2), the adjusting disc (6-4) is fixedly connected to the circle center of the lower top end surface of the threaded column (6-2), and the support block (6-1) is fixedly connected to the middle of the upper edge of the front top end surface of the movable rotating block (5).
4. The support device for aircraft parts machining according to claim 1, characterized in that: the fixing device (7) comprises a clamping block (7-1), a pressing plate (7-2) and bolts (7-3), the clamping block (7-1) is in a concave shape, the pressing plate (7-2) is inserted above the inside of the clamping block (7-1), the bolts (7-3) are respectively inserted in the middle of the edge of the top end surface of the clamping block (7-1), and the bolts (7-3) penetrate through the upper surface of the clamping block (7-1) and are inserted in the upper surface of the pressing plate (7-2).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922442834.9U CN211639611U (en) | 2019-12-30 | 2019-12-30 | Supporting device for airplane part machining |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922442834.9U CN211639611U (en) | 2019-12-30 | 2019-12-30 | Supporting device for airplane part machining |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN211639611U true CN211639611U (en) | 2020-10-09 |
Family
ID=72701180
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201922442834.9U Active CN211639611U (en) | 2019-12-30 | 2019-12-30 | Supporting device for airplane part machining |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN211639611U (en) |
-
2019
- 2019-12-30 CN CN201922442834.9U patent/CN211639611U/en active Active
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